01-284-0603
Wing Section Center Rib
01-284-0604
Aircraft Stringer
01-284-1613
Structural Aircraft Plate
Used on C-130. 17.700" overall length 2.930" overall width 2.340" material thickness
01-284-1614
Structural Aircraft Plate
Used on C-130. 17.700" overall length 2.930" overall width 2.340" material thickness
01-284-1615
Structural Component Air Support
Used on f-16c/d aircraft.
01-284-2600
Structural Aircraft Plate
Used on acft model e-3a. 2024-T3511 extr per qq-a-200/3, T3511 temp; finish SRF2.30; alter AND10136-1407 by 11.0 in lg; nha 65-60900
01-284-2601
Structural Aircraft Plate
Used on acft model kc-135. clad 2024-0 sheet per qq-a-362, otemper; heat treat T4; finish SRF2.115; 37.0 in lg, 1.0 in wd, 0.040 in thk
01-284-2654
Structural Aircraft Plate
01-284-2655
Structural Component Air Support
01-284-3503
Structural Component Air Support
Used on acft,model av8.
01-284-3504
Structural Component Air Support
Used on acft,model av8.
01-284-3527
Airfoil Rib
10.000" overall length 5.000" overall width 0.040" material thickness nha -1001
01-284-3528
Airfoil Rib
10.000" overall length 5.000" overall width 0.040" material thickness nha -1001
01-284-3529
Airfoil Rib
10.500" overall length 5.000" overall width 0.040" material thickness nha -1001
01-284-3530
Airfoil Rib
10.500" overall length 5.000" overall width 0.040" material thickness nha -1001
01-284-3608
Thermal Special Purpo Insulation
L-h; u/o environment control system-aft fuselage f-15 acft
01-284-3612
Fluid Aircraft Manifold
Consist of 1 weld assy, 2 ferrule, 8 insert; located YF610.; used as weapons bay tank to main tank fwd fuel vent tube manifold assembly; acft b-1b
01-284-3613
Fluid Aircraft Manifold
Consist of 1 weld assy, 2 ferrule, marking a/r; located YF547; used as fwd fuel tank vent manifold; acft model b-1b
01-284-5089
Access Aircraft Door
Used on aircraft model f-18.
01-284-5090
Access Aircraft Door
Used on a-6e acft.
01-284-5091
Access Aircraft Door
Used on aircraft model f-18.
01-284-5092
Access Aircraft Door
Used on aircraft model f-18.
01-284-5093
Access Aircraft Door
Used on aircraft model f-18.
01-284-5094
Access Aircraft Door
Used on aircraft model f-18.
01-284-5146
Aircraft Pylon
Used on a-6e acft.
01-284-5147
Aircraft Pylon
Used on a-6e acft.
01-284-5395
Structural Aircraft Plate
Used on c-5 aircraft. plate-serrated, aft cargo door, uplock, scm, mod kit; size .160X4X5; space cargo mods
01-284-6415
Structural Aircraft Plate
01-284-6416
Structural Component Air Support
01-284-6420
Aircraft Door
Used on ah-64 apache airframe.
01-284-6427
Structural Aircraft Panel
Used on e-3a aircraft. skin panel-honeycomb, upper & lower outboard halves, outboard aileron
01-284-6429
Structural Aircraft Panel
Used on e-3a aircraft. part of panel assembly, upper outboard, aft
01-284-6430
Structural Aircraft Panel
Used on e-3a aircraft. panel assembly, upper outbd, aft
01-284-6431
Structural Aircraft Panel
Used on e-3a aircraft. panel assembly, upper skin
01-284-6432
Structural Aircraft Panel
Used on e-3a aircraft. panel, upper aft skin
01-284-6433
Structural Aircraft Panel
Used on e-3a aircraft. panel, upper aft skin
01-284-6434
Aircraft Skin
Used on e-3a aircraft. matl 2024-T3 al clad sh per qq-a-362; size .040X6.0X99.5; part of aileronassembly-outboard wing
01-284-6435
Aircraft Trailing Edge
01-284-7210
Structural Component Air Support
Used on c-5 aircraft. link-pressure door seal, scm, modkit; matl 7075-T7351 bare per qq-a-250/12; size .375X1X2; nha 4F59387; space cargo mods
01-284-7211
Structural Component Air Support
Used on c-5 aircraft. link-pressure door seal, scm, modkit; matl 7075-T7351 bare per qq-a-250/12; size .375X1X2; nha 4F59387; space cargo mods
01-284-7354
Structural Component Air Support
01-284-7356
Structural Component Air Support
01-284-8437
Structural Aircraft Plate
Used on acft model e-3a.
01-284-8438
Structural Aircraft Plate
Used on acft model b-1b. PH13-8mo cres bar, cond a per ST0160LB0013; 1.56 in lg, 1.25 in wd, 0.375 in thk; nha L3226420; heat treat ST0111LA0008 to cond H1000; finish 60HA02
01-284-8439
Structural Aircraft Plate
Used on acft model b-1b. PH13-8M0 cres bar cond a per ST0160LB0013, 1.46 in lg, 1.25 in wd, 0.375 in thk; heat treat ST0111LA0008 to cond H1000; finish 60HA02; nha L3226420
01-284-8440
Structural Aircraft Plate
Used on acft model b-1b. PH13-8M0 cres bar cond a per ST0160LB0013, 2.31 in lg, 2.00 in wd, 0.500 in thk; heat treat ST0111LA0008 to cond H1000; finish 60HA02; nha L3226420
01-284-8441
Structural Aircraft Plate
Used on b-1b b0mber airplane.... 2.310" overall length 2.000" overall width 0.500" material thickness nha; L3226420, heat treat ST0111LA0008 to cond H1000, PH13-8mo cres bar cond a per AT0160LB0013,
01-284-8442
Structural Aircraft Plate
Used on F-15. web
